As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SLAT FAILED AT 0 DURING CLIMB OUT AT 5500 FT WITH SLAT/FLAPS AT 0/0. ACCOMPLISHED ELECTRICAL CK OF THE OB SLAT SKEW SENSOR AND WIRE HARNESS. IAW FIM 27-83-00-810-814-A. REPLACED FAULTED RT WIRE HARNESS (W612) IAW M/M 27-83-07 FOR SLATS 3/4 SKEW SENSOR. OPERATION CKS NORMAL. FAIL MSG CLEARED.